Back-pressure effects on unsteadiness of separation shock in a rectangular duct at Mach 3 - Concepedia

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Back-pressure effects on unsteadiness of separation shock in a rectangular duct at Mach 3

34

Citations

25

References

2017

Year

Bing Xiong, Xiaoqiang Fan, Yi Wang, Liang Zhou, Yuan Tao

Acta Astronautica

Mach 3Rectangular DuctCompressible FlowUnsteady FlowEngineeringAerospace EngineeringFluid MechanicsMechanical EngineeringAerodynamicsSeparation ShockBoundary LayerShock Compression

References

	Year	Citations

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